View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 41169U 15077D 25177.62803816 .04978187 -27512-4 80740-3 0 9995
2 41169 14.9820 136.7861 0000764 246.8638 291.1774 16.32314160529153
| Epoch (UTC): | 26 June 2025 15:04:22 |
| Eccentricity: | 0.0000764 |
| inclination: | 14.9820° |
| perigee height: | 186 km |
| apogee height: | 187 km |
| right ascension of ascending node: | 136.7861° |
| argument of perigee: | 246.8638° |
| revolutions per day: | 16.32314160 |
| mean anomaly at epoch: | 291.1774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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